Acoustic characteristics of a large-scale wind-tunnel model of a jet flap aircraft /

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Acoustic and aerodynamic study of a pusher-propeller aircraft model /

Soderman, Paul T.
Horne, W. Clifton (William Clifton)
Ames Research Center.

January 1990

Prepared at Ames Research Center.Bibliography: p. 13-14.Mode of access: Internet

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Numerical study of sound propagation in a jet flow /

Padula, Sharon L.
Liu, Chen-Huei.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

Acoustic measurements from a rotor blade-vortex interaction noise experiment in the German-Dutch wind tunnel (DNW) /

Martin, R. M. (Ruth McVoy), 1956-
United States. Army Aviation Research and Technology Activity.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"March 1988"--Cover."US Army Aviation Systems Command, Aviation R&T Activity"--Cover.Bibliography: p...

Results of full-scale wind tunnel tests on the H.126 jet flap aircraft /

Aiken, Thomas N.
Cook, Anthony, M.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 4.Mode of access: Internet

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Noise characteristics of jet flap type exhaust flows /

Schrecker, G. O.
Maus, J. R.
Langley Research Center.
University of Tennessee (System). Space Institute.

January 1974

"Prepared by the University of Tennessee Space Institute ... for Langley Research Center."Cover titl...

Wind-tunnel investigation of internally blown jet-flap STOL airplane model /

Vogler, Raymond D.
United States. National Aeronautics and Space Administration.

January 1976

Issued Nov. 1976.Includes bibliographical references (p. 8).Mode of access: Internet

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of several sonic inlet takeoff and approach geometries /

Abbott, John M.
Golladay, Richard L.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20-21).Mode of...

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Large-scale wind-tunnel tests of an airplane model with two propellers and rotaing cylinder flaps /

Weiberg, James A.
Gamse, Berl.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 9).Mode of access: Internet

Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model /

Feistel, Terrell W.
Morelli, Joseph P.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Aeromechanics Laboratory, AVRADCOM Research and Technology Laboratories, Ames Re...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Acoustic and aerodynamic study of a pusher-propeller aircraft model /

Soderman, Paul T.
Horne, W. Clifton (William Clifton)
Ames Research Center.

January 1990

Prepared at Ames Research Center.Bibliography: p. 13-14.Mode of access: Internet

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

Numerical study of sound propagation in a jet flow /

Padula, Sharon L.
Liu, Chen-Huei.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ...

Acoustic measurements from a rotor blade-vortex interaction noise experiment in the German-Dutch wind tunnel (DNW) /

Martin, R. M. (Ruth McVoy), 1956-
United States. Army Aviation Research and Technology Activity.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

January 1988

"March 1988"--Cover."US Army Aviation Systems Command, Aviation R&T Activity"--Cover.Bibliography: p...

Results of full-scale wind tunnel tests on the H.126 jet flap aircraft /

Aiken, Thomas N.
Cook, Anthony, M.
Ames Research Center.

January 1973

Prepared at Ames Research Center.Cover title.Bibliography: p. 4.Mode of access: Internet

Wind-tunnel investigation of a twin-engine straight-wing upper-surface blown jet-flap configuration /

Phelps, Arthur E.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Noise characteristics of jet flap type exhaust flows /

Schrecker, G. O.
Maus, J. R.
Langley Research Center.
University of Tennessee (System). Space Institute.

January 1974

"Prepared by the University of Tennessee Space Institute ... for Langley Research Center."Cover titl...

Wind-tunnel investigation of internally blown jet-flap STOL airplane model /

Vogler, Raymond D.
United States. National Aeronautics and Space Administration.

January 1976

Issued Nov. 1976.Includes bibliographical references (p. 8).Mode of access: Internet

Low-speed wind-tunnel investigation of the aerodynamic and acoustic performance of several sonic inlet takeoff and approach geometries /

Abbott, John M.
Golladay, Richard L.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20-21).Mode of...

Wind-tunnel investigation of an upper surface blown jet-flap powered-lift configuration /

Phelps, Arthur E.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 11).Mode of ...

Large-scale wind-tunnel tests of an airplane model with two propellers and rotaing cylinder flaps /

Weiberg, James A.
Gamse, Berl.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 9).Mode of access: Internet

Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model /

Feistel, Terrell W.
Morelli, Joseph P.
Aeromechanics Laboratory.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Aeromechanics Laboratory, AVRADCOM Research and Technology Laboratories, Ames Re...

Full-scale wind-tunnel investigation of the aerodynamic characteristics of the X-24A lifting body aircraft /

Mort, Kenneth W.
Falarski, Michael D.
U.S. Army Aeronautical Research Laboratory.
Ames Research Center.
United States. National Aeronautics and Space Administration.

"August 1970."Cover title.Includes bibliographical references (p. 6).Mode of access: Internet

Aerodynamic characteristics of a 1/6-scale model of the rotor systems research aircraft with the rotors removed /

Mineck, Raymond E.
Hassell, James L., joint author.
Freeman, Carl E., joint author.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1976

Cover title.Includes bibliographical references (p. 23).Mode of access: Internet

Aeroacoustic wind-tunnel tests of a light twin-boom general aviation airplane with free or shrouded-pusher propellers /

McLemore, H. Clyde.
Pegg, Robert J.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"April 1980"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Acoustic characteristics of a large-scale wind-tunnel model of a jet flap aircraft /

Abstract

Extracted data

Acoustic characteristics of a large-scale wind-tunnel model of a jet flap aircraft /

Abstract

Extracted data

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